摘要
针对四旋翼飞行器高度控制通道易受干扰的问题,在先验飞行数据基础上,利用局部加权线性回归算法建立了四旋翼飞行器的非参数模型,该模型考虑了实际飞行中干扰因素对高度控制的影响。以此非参数模型为基础,运用强化学习算法构建了四旋翼飞行器高度控制算法,并以离线方式优化了控制算法的结构参数。最后通过实际的飞行实验验证了控制算法的合理性。
To solve the problem that the quadrotor aircraft height control channel is susceptible to be interfered, on the basis of a priori flight data, a non-parametric model of quadrotor aircraft is established by using the locally weighted linear regression algorithm, which considers the influence of interference factors on the height control in actual flight. Based on this non-parametric model, a quadrotor aircraft height control algorithm is constructed by using reinforcement learning algorithm and the structural parameters of the control algorithm is optimized in offline mode. Finally, the actual flight experiment validated the control algorithm.
出处
《测控技术》
CSCD
2016年第10期51-53,58,共4页
Measurement & Control Technology
关键词
四旋翼飞行器
局部加权线性回归
非参数模型
强化学习
quadrotor aircraft
locally weighted linear regression
non-parametric model
reinforcement learning algorithm